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https://bitbucket.org/librepilot/librepilot.git
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7d66a075de
1. Fix autoyaw to 0 attitude on takeoff post launch. 2. An error condition abort now properly disarms and continues to contrain thrust and stabi during disarmed state. 3. Increase thrustdown time from 2 to 5 seconds on an error condition (e.g. if 3 m deviation from takeoff position on NE).
154 lines
5.1 KiB
C++
154 lines
5.1 KiB
C++
/**
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******************************************************************************
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* @addtogroup OpenPilotModules OpenPilot Modules
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* @{
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* @addtogroup PathFollower FSM
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* @brief Executes landing sequence via an FSM
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* @{
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*
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* @file vtollandfsm.h
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* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2015.
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* @brief Executes FSM for landing sequence
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*
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* @see The GNU Public License (GPL) Version 3
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*
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*****************************************************************************/
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/*
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* This program is free software; you can redistribute it and/or modify
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* it under the terms of the GNU General Public License as published by
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* the Free Software Foundation; either version 3 of the License, or
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* (at your option) any later version.
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*
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* This program is distributed in the hope that it will be useful, but
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* WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY
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* or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
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* for more details.
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*
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* You should have received a copy of the GNU General Public License along
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* with this program; if not, write to the Free Software Foundation, Inc.,
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* 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA
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*/
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#ifndef VTOLAUTOTAKEOFFFSM_H
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#define VTOLAUTOTAKEOFFFSM_H
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extern "C" {
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#include "statusvtolautotakeoff.h"
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}
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#include "pathfollowerfsm.h"
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// AutoTakeoffing state machine
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typedef enum {
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AUTOTAKEOFF_STATE_INACTIVE = 0, // Inactive state is the initialised state on startup
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AUTOTAKEOFF_STATE_CHECKSTATE, // Initial condition checks
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AUTOTAKEOFF_STATE_SLOWSTART, // Slow start motors
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AUTOTAKEOFF_STATE_THRUSTUP, // Ramp motors up to neutral thrust
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AUTOTAKEOFF_STATE_TAKEOFF, // Ascend to target velocity
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AUTOTAKEOFF_STATE_HOLD, // Hold position as completion of the sequence
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AUTOTAKEOFF_STATE_THRUSTDOWN, // Thrust down sequence
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AUTOTAKEOFF_STATE_THRUSTOFF, // Thrust is now off
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AUTOTAKEOFF_STATE_DISARMED, // Disarmed
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AUTOTAKEOFF_STATE_ABORT, // Abort on error triggerig fallback to hold
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AUTOTAKEOFF_STATE_SIZE
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} PathFollowerFSM_AutoTakeoffState_T;
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class VtolAutoTakeoffFSM : public PathFollowerFSM {
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private:
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static VtolAutoTakeoffFSM *p_inst;
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VtolAutoTakeoffFSM();
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public:
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static VtolAutoTakeoffFSM *instance()
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{
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if (!p_inst) {
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p_inst = new VtolAutoTakeoffFSM();
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}
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return p_inst;
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}
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int32_t Initialize(VtolPathFollowerSettingsData *vtolPathFollowerSettings,
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PathDesiredData *pathDesired,
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FlightStatusData *flightStatus);
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void Inactive(void);
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void Activate(void);
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void Update(void);
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void BoundThrust(float &ulow, float &uhigh);
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PathFollowerFSMState_T GetCurrentState(void);
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void ConstrainStabiDesired(StabilizationDesiredData *stabDesired);
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uint8_t PositionHoldState(void);
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void setControlState(StatusVtolAutoTakeoffControlStateOptions controlState);
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protected:
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// FSM instance data type
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typedef struct {
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StatusVtolAutoTakeoffData fsmAutoTakeoffStatus;
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StatusVtolAutoTakeoffStateOptions currentState;
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TakeOffLocationData takeOffLocation;
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uint32_t stateRunCount;
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uint32_t stateTimeoutCount;
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float sum1;
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float sum2;
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float expectedAutoTakeoffPositionNorth;
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float expectedAutoTakeoffPositionEast;
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float thrustLimit;
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float boundThrustMin;
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float boundThrustMax;
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uint8_t observationCount;
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uint8_t observation2Count;
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uint8_t flZeroStabiHorizontal;
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uint8_t flConstrainThrust;
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uint8_t flLowAltitude;
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uint8_t flAltitudeHold;
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} VtolAutoTakeoffFSMData_T;
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// FSM state structure
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typedef struct {
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void(VtolAutoTakeoffFSM::*setup) (void); // Called to initialise the state
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void(VtolAutoTakeoffFSM::*run) (uint8_t); // Run the event detection code for a state
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} PathFollowerFSM_AutoTakeoffStateHandler_T;
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// Private variables
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VtolAutoTakeoffFSMData_T *mAutoTakeoffData;
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VtolPathFollowerSettingsData *vtolPathFollowerSettings;
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PathDesiredData *pathDesired;
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FlightStatusData *flightStatus;
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void setup_inactive(void);
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void setup_checkstate(void);
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void setup_slowstart(void);
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void run_slowstart(uint8_t);
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void setup_takeoff(void);
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void run_takeoff(uint8_t);
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void setup_hold(void);
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void run_hold(uint8_t);
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void setup_thrustup(void);
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void run_thrustup(uint8_t);
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void setup_thrustdown(void);
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void run_thrustdown(uint8_t);
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void setup_thrustoff(void);
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void run_thrustoff(uint8_t);
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void setup_disarmed(void);
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void run_disarmed(uint8_t);
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void initFSM(void);
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void setState(StatusVtolAutoTakeoffStateOptions newState, StatusVtolAutoTakeoffStateExitReasonOptions reason);
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int32_t runState();
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int32_t runAlways();
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void updateVtolAutoTakeoffFSMStatus();
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void assessAltitude(void);
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void setStateTimeout(int32_t count);
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static PathFollowerFSM_AutoTakeoffStateHandler_T sAutoTakeoffStateTable[AUTOTAKEOFF_STATE_SIZE];
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};
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#endif // VTOLAUTOTAKEOFFFSM_H
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